Title :
A Direct Method for Enforcing Equality Constraints in Optimal Output Feedback
Author :
Raman, Kidambi V. ; Calise, Anthony J.
Author_Institution :
RCA Astro Electronics Co., P.O. Box 800, Princeton, NJ 08540
Abstract :
This paper presents an algorithm that can be used to calculate optimal output feedback gains subject to a linear constraint on the gain matrix. This method is direct in that it does not rely on a penalty function approach. The algorithm is proven to converge to a local minimum. As an application, the lateral dynamics of an L-1011 aircraft are considered both for static gain output feedback and dynamic compensator design.
Keywords :
Aerodynamics; Aerospace engineering; Aircraft; Algorithm design and analysis; Control systems; Convergence; Gain; Linear feedback control systems; Output feedback; Performance analysis;
Conference_Titel :
American Control Conference, 1986
Conference_Location :
Seattle, WA, USA